IL187799A - Rotor blade for a high speed rotary wing aircraft - Google Patents

Rotor blade for a high speed rotary wing aircraft

Info

Publication number
IL187799A
IL187799A IL187799A IL18779907A IL187799A IL 187799 A IL187799 A IL 187799A IL 187799 A IL187799 A IL 187799A IL 18779907 A IL18779907 A IL 18779907A IL 187799 A IL187799 A IL 187799A
Authority
IL
Israel
Prior art keywords
rotor blade
main rotor
region
main
chord
Prior art date
Application number
IL187799A
Other languages
English (en)
Other versions
IL187799A0 (en
Original Assignee
Sikorsky Aircraft Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sikorsky Aircraft Corp filed Critical Sikorsky Aircraft Corp
Publication of IL187799A0 publication Critical patent/IL187799A0/en
Publication of IL187799A publication Critical patent/IL187799A/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/08—Helicopters with two or more rotors
    • B64C27/10—Helicopters with two or more rotors arranged coaxially
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/467—Aerodynamic features
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8236—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft including pusher propellers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/02—Formulas of curves
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/05—Variable camber or chord length

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Wind Motors (AREA)
IL187799A 2005-05-31 2007-12-02 Rotor blade for a high speed rotary wing aircraft IL187799A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/140,706 US7252479B2 (en) 2005-05-31 2005-05-31 Rotor blade for a high speed rotary-wing aircraft
PCT/US2006/016639 WO2007086908A2 (fr) 2005-05-31 2006-04-28 Pale de rotor pour aéronef à voilure tournante de vitesse élevée

Publications (2)

Publication Number Publication Date
IL187799A0 IL187799A0 (en) 2008-08-07
IL187799A true IL187799A (en) 2012-05-31

Family

ID=37463585

Family Applications (1)

Application Number Title Priority Date Filing Date
IL187799A IL187799A (en) 2005-05-31 2007-12-02 Rotor blade for a high speed rotary wing aircraft

Country Status (8)

Country Link
US (1) US7252479B2 (fr)
EP (1) EP1893483B1 (fr)
JP (1) JP5078883B2 (fr)
CN (1) CN101501302B (fr)
CA (1) CA2609940C (fr)
IL (1) IL187799A (fr)
RU (1) RU2408499C2 (fr)
WO (1) WO2007086908A2 (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7854593B2 (en) * 2006-02-16 2010-12-21 Sikorsky Aircraft Corporation Airfoil for a helicopter rotor blade
PT2123556E (pt) * 2008-05-22 2011-02-04 Agusta Spa Pá do rotor da cauda anti-torque para helicóptero
US8167567B2 (en) 2008-12-17 2012-05-01 United Technologies Corporation Gas turbine engine airfoil
JP5693842B2 (ja) * 2009-12-14 2015-04-01 独立行政法人 宇宙航空研究開発機構 ヘリコプタのロータ・ブレード
EP2505500B1 (fr) * 2011-03-31 2016-09-14 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Pale de rotor à bruit et performance améliorés pour hélicoptère
US9017036B2 (en) 2012-02-29 2015-04-28 United Technologies Corporation High order shaped curve region for an airfoil
US9845683B2 (en) 2013-01-08 2017-12-19 United Technology Corporation Gas turbine engine rotor blade
US9656747B2 (en) * 2013-03-14 2017-05-23 Bell Helicopter Textron Inc. Soft in-plane and stiff out-of-plane rotor system
US9688395B2 (en) * 2013-12-04 2017-06-27 Sikorsky Aircraft Corporation Boundary layer ingesting blade
US10288399B2 (en) 2014-07-01 2019-05-14 Sikorsky Aircraft Corporation Blade geometry characterization tool
WO2016053408A1 (fr) 2014-10-01 2016-04-07 Sikorsky Aircraft Corporation Variation de signature acoustique d'aéronef mettant en oeuvre un embrayage
EP3201077B1 (fr) 2014-10-01 2020-05-20 Sikorsky Aircraft Corporation Aéronef à voilure tournante et à deux rotors
JP2017100620A (ja) * 2015-12-03 2017-06-08 国立研究開発法人宇宙航空研究開発機構 ヘリコプタ、ブレード及びロータ
DE102015121502A1 (de) * 2015-12-10 2017-06-14 Christoph Fraundorfer Tragschrauberrotorblatt zur autorotatorischen Auftriebserzeugung
FR3045564B1 (fr) 2015-12-21 2018-08-17 Airbus Helicopters Pale de rotor d'aeronef a geometrie adaptee pour l'amelioration acoustique lors de vols d'approche et l'amelioration des performances en vols stationnaire et d'avancement
FR3045565B1 (fr) * 2015-12-21 2018-07-27 Airbus Helicopters Pale de rotor d'aeronef a geometrie adaptee pour l'ameloration acoustique lors d'un vol d'approche et l'amelioration des performances en vol d'avancement
WO2017172000A2 (fr) * 2016-01-29 2017-10-05 Sikorsky Aircraft Corporation Pales de rotor de queue d'hélicoptère et ensembles pales
JP6980962B2 (ja) * 2017-04-26 2021-12-15 国立研究開発法人宇宙航空研究開発機構 メインロータブレード及びヘリコプタ
RU2692328C2 (ru) * 2017-06-19 2019-06-24 Борис Андреевич Половинкин Лопасти несущего винта для автожира и вертолета с переменной круткой
JP6953322B2 (ja) * 2018-02-01 2021-10-27 本田技研工業株式会社 ファンブレードの形状決定方法
US11999466B2 (en) * 2019-11-14 2024-06-04 Skydio, Inc. Ultra-wide-chord propeller
CN112173075B (zh) * 2020-09-25 2022-12-30 中国直升机设计研究所 一种直升机低噪声旋翼桨叶气动外形
US12116119B2 (en) * 2022-03-28 2024-10-15 Lockheed Martin Corporation High speed rotor blade design
CN116443244B (zh) * 2023-04-16 2023-09-29 西北工业大学 一种用于前行桨叶概念高速直升机桨叶尖部的高升阻比超临界翼型

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR411538A (fr) * 1910-01-13 1910-06-18 Alexandre Fougeron Hélice pour la navigation aérienne
US1692081A (en) * 1925-11-24 1928-11-20 Cierva Juan De La Aircraft with rotative wings
US1990291A (en) * 1931-12-05 1935-02-05 Autogiro Co Of America Air-rotor for aircraft
US3116040A (en) * 1961-06-26 1963-12-31 Us Industries Inc Supersonic rotary wing platform
US4130377A (en) * 1977-07-13 1978-12-19 United Technologies Corporation Helicopter blade and rotor
US4248572A (en) * 1978-12-11 1981-02-03 United Technologies Corporation Helicopter blade
EP0037633B1 (fr) * 1980-03-28 1986-07-30 WESTLAND plc Pale de rotor pour hélicoptère
FR2617118B1 (fr) * 1987-06-29 1992-08-21 Aerospatiale Pale a extremite courbe pour voilure tournante d'aeronef
FR2636593B1 (fr) * 1988-09-19 1990-11-23 Aerospatiale Pale pour voilure tournante d'aeronef et voilure tournante comportant une telle pale
US5137427A (en) * 1990-12-20 1992-08-11 United Technologies Corporation Quiet tail rotor
FR2689852B1 (fr) * 1992-04-09 1994-06-17 Eurocopter France Pale pour voilure tournante d'aeronef, a extremite en fleche.
US5277380A (en) * 1992-06-22 1994-01-11 United Technologies Corporation Toroidal fuselage structure for unmanned aerial vehicles having ducted, coaxial, counter-rotating rotors
US5879131A (en) * 1994-04-25 1999-03-09 Arlton; Paul E. Main rotor system for model helicopters
FR2755941B1 (fr) * 1996-11-19 1999-01-15 Eurocopter France Pale a extremite en fleche pour voilure tournante d'aeronef
US5782607A (en) * 1996-12-11 1998-07-21 United Technologies Corporation Replaceable ceramic blade insert
FR2768121B1 (fr) * 1997-09-10 1999-11-19 Onera (Off Nat Aerospatiale) Pale a signature sonore reduite, pour voilure tournante d'aeronef, et voilure tournante comportant une telle pale
FR2793766B1 (fr) * 1999-05-21 2001-07-13 Eurocopter France Pale pour voilure tournante d'aeronef

Also Published As

Publication number Publication date
RU2408499C2 (ru) 2011-01-10
IL187799A0 (en) 2008-08-07
EP1893483A4 (fr) 2014-11-05
WO2007086908A3 (fr) 2009-04-16
CN101501302A (zh) 2009-08-05
JP5078883B2 (ja) 2012-11-21
CN101501302B (zh) 2012-06-20
US20060269418A1 (en) 2006-11-30
US7252479B2 (en) 2007-08-07
EP1893483A2 (fr) 2008-03-05
CA2609940C (fr) 2010-08-17
RU2007148890A (ru) 2009-07-10
EP1893483B1 (fr) 2017-10-11
JP2008542110A (ja) 2008-11-27
CA2609940A1 (fr) 2007-08-02
WO2007086908A2 (fr) 2007-08-02

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